▸Orbital parameters

Orbit class	SSO
Inclination	97.7759°
Eccentricity	0.0001731
Period	96.2 min
Apogee	579 km
Perigee	577 km
Mean motion	14.96400428 rev/day
RAAN	302.8780°
Arg of perigee	101.1147°
Mean anomaly	259.0269°
B*	3.8771e-4
Rev at epoch	5,690

▸Two-line element set (TLE)

EPOCH Jul 7, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 64561U 25135AK 26188.13632123 .00004336 00000-0 38771-3 0 9999

2 64561 97.7759 302.8780 0001731 101.1147 259.0269 14.96400428 56904

▸ source OMM (JSON)

{
  "OBJECT_NAME": "LEMUR-2-KRISH",
  "OBJECT_ID": "2025-135AK",
  "EPOCH": "2026-07-07T03:16:18.154+00:00",
  "MEAN_MOTION": 14.96400428,
  "ECCENTRICITY": 0.0001731,
  "INCLINATION": 97.7759,
  "RA_OF_ASC_NODE": 302.878,
  "ARG_OF_PERICENTER": 101.1147,
  "MEAN_ANOMALY": 259.0269,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 64561,
  "REV_AT_EPOCH": 5690,
  "BSTAR": 0.00038771,
  "MEAN_MOTION_DOT": 0.00004336,
  "MEAN_MOTION_DDOT": 0
}

Reconstructed from CelesTrak OMM mean-elements (element-set number is a placeholder). TLE/OMM data is approximate. Not for operational use or collision avoidance.

▸Satellite metadata

Name	LEMUR-2-KRISH
Operator	Spire / Mission Control Space ServicesHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Jun 23, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	10HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—
Object class	PAYLOADHIGH

▸Data quality

Score85 / 100

Claims7

Sources1

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org

▸Actions

GET /api/v1/satellites/64561

//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.